With increased power and lighter components requirements,
engineers must take into account aero-elastic effects for
state-of-the-art turbomachinery analysis. Flutter is a self-
excited and self-sustained aero-elastic instability phenomenon
that leads to fatigue and damage. Its investigation can be
carried out by computing the aerodynamic damping of the
structure.
FINE/Turbo introduces the modal approach, a novel and
efficient method for fluid structure interaction prediction
covering cold-to-hot, forced response and flutter analysis.
Join us for this FREE webinar and discover how you can take
benefit from the modal approach implemented in FINE/Turbo.
Registration & Timing:
Duration: approx. 30 minutes

Event record first posted on December 20, 2013, last modified on January 9, 2014